IEEE - Institute of Electrical and Electronics Engineers, Inc. - Investigation of the effect of thickness, taper ratio and aspect ratio on fin flutter velocity of a model rocket using response surface method

2015 7th International Conference on Recent Advances in Space Technologies (RAST)

Author(s): Ceyhun Tola ; Melike Nikbay
Publisher: IEEE - Institute of Electrical and Electronics Engineers, Inc.
Publication Date: 1 June 2015
Conference Location: Istanbul, Turkey
Conference Date: 16 June 2015
Page(s): 27 - 32
ISBN (Electronic): 978-1-4799-7697-3
ISBN (Paper): 978-1-4673-7760-7
DOI: 10.1109/RAST.2015.7208310
Regular:

The main focus of this study is to examine the effect of thickness, taper ratio and aspect ratio on the fin flutter speed of a model rocket using response surface method. The most effective... View More

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